I believe we should use Mirek's command receiver on L band as adapted
for our purposes. If we want a redundant one for any reason, we do
that one on 70cm. The command receiver should feed the IHU-3 SDR for
any normal commanding and any reset vector decoder we choose to enable.
The issue is straightforward. Any module that needs a heat sink will
have been designed to be kept cool when the spacecraft is receiving a
large thermal input from the sun. When this thermal input is removed,
the same radiation cooling that was keeping the module cool will
continue to operate irrespective of the solar input. That module will
get cold over time. If the bottom temperature stops the unit from
operating properly and it is a command receiver, this is not a good
thing. I believe we should have dedicated command receivers anyway and
these to do not need 80 dB of dynamic range and can be made narrow
band. Our solar eclipse pattern has been given a preliminary analysis
for the proposed orbit and we will be subjected to eclipses of
insufficient duration to cause us severe thermal problems but what
thermal issues there are need to be understood and this is what Dick is
warning us about. This analysis of the eclipse pattern was also the
basis of my analysis that it would take well over a decade to subject
any Li-ion battery to sufficient cycles to worry about.
Bob
N4HY
John B. Stephensen wrote:
The SAW filters work down to -35 C and the ICs to -40 C so its not too
far off. It's easy to use a lower power RF amplifier and mixer which
will lower the input intercept. Right now, the receiver is designed to
tolerate direct hits from PAVE PAWS at any two frequencies outside the
IF passband. As the input intecept is lowered, the percentage of
pulses that cause interference increases, but the receiver won't go
completely deaf as was reported on earlier satelites.
73,
John
KD6OZH
----- Original Message -----
*From:* Dick Jansson-rr <mailto:rjansson@cfl.rr.com>
*To:* AMSAT Eagle <mailto:eagle@amsat.org>
*Sent:* Wednesday, October 11, 2006 17:51 UTC
*Subject:* [eagle] Module Temperatures
Last evening I tried to convey the concept that the
critical-command modules needed to be of low-power design to
insure their operability during the occasional rather lengthy
eclipse cooling of the spacecraft. My message apparently did not
sink in. John reports that his design of such a U band receiver
would be dissipating some 3.5W due to its bullet-proof nature
against 3rd-order IM products needed for protection on the U band.
If we go forward with such a module of that nature, it will need
to have thermal control tapes on it to provide a mean emittance of
about e=0.45. In a 3 hour eclipse we can expect to see spaceframe
temperatures down to -100°C (173K) or lower. With such an
environment John's module would be expected to see temperatures
down to at least -44°C, which is a bit frosty for electronics that
are expected to provide the critical services of commanding the
spacecraft. Such operating temperatures are not felt to be
advisable for that service.
If John's module were of the 1W category, temperatures of the
receiver could be expected to be in the range of -15°C to -20°C
which would be more operable for the service.
The above numbers are, of course, based on estimates which will be
confirmed after we have the new spaceframe fully designed and
analyzed. The "warmer" temperatures of the lower power modules are
those that have been experienced and measured by telemetry from
AO-10 and AO-13. These projections are thus based on 25 years of
experience in these design concepts.
/Dick Jansson/
_---------------------------_
rjansson@cfl.rr.com <mailto:rjansson@cfl.rr.com>
_---------------------------_
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